US2793784A - Test plug for pressure vessels - Google Patents

Test plug for pressure vessels Download PDF

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Publication number
US2793784A
US2793784A US564017A US56401756A US2793784A US 2793784 A US2793784 A US 2793784A US 564017 A US564017 A US 564017A US 56401756 A US56401756 A US 56401756A US 2793784 A US2793784 A US 2793784A
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Prior art keywords
shaft
gland
lug
aperture
test plug
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US564017A
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Robert L Mcinnes
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Griscom Russell Co
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Griscom Russell Co
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M3/00Investigating fluid-tightness of structures
    • G01M3/02Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
    • G01M3/32Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
    • G01M3/3227Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators for radiators

Definitions

  • This invention relates to a test plug and more pa-rticularly it pertains to a quick opening closure for openings in a heat exchanger for testing purposes.
  • Heat exchangers are provided with inlets and outlets for the passage of heat exchange fluids as well as other openings for various other purposes. Such openings are usually used for the connection of instruments, such as gage glasses and pressure valves.
  • test pressure at least equal to one and one-half times the design pressure is usually required by construction codes. In order to apply the test pressures all openings must be closed of, except one opening through which the test tiuid is pumped into the pressure vessel.
  • Another object of this invention is to provide a test plug for the -openings in a heat exchanger that is manually operated without the aid of tools.
  • the nature of the improvedv test plug construction of the present invention may be stated in general terms as including a shaft having a threaded end and having a lug at the other end, the lug having a lateral dimension greater than the diameter of the shaft and smaller than the diameter of tne opening in a pressure vessel.
  • a necked portion is provided on the shaft adjacent the lug, and a crescent-shaped snap ring is rotatably mounted on the necked portion having a diameter less than that of the opening.
  • An annular member is rotatably mounted on the shaft between the necked portion and the threaded end, the member having a portion of diameter smaller than that of the pressurevessel opening and having a circumferential groove around said portion with a resilient gasket partially seated therein for engagement with the opening, and a nut mounted on the threaded end of the shaft for tightening the assembly in the opening.
  • Fig. 1 is a vertical sectional View through a heat exchanger showing one embodiment of the present invention installed therein;
  • Fig. 2 is a perspective view of the device
  • Fig. 3 is a vertical sectional view showing thedevice partially installed in an opening in a heat exchanger
  • Fig. 4 is a horizontal sectional View taken on the line 4-4 of Fig. 3;
  • Fig. 5 is a vertical sectional view showing the device fully installed in the opening
  • Fig. 6 is a horizontal sectional view taken on the line 6-6 of Fig. 5;
  • Fig. 7 is a horizontal sectional View taken on the line 7-7' of Fig. 5;
  • Fig. 8 is a vertical sectional view of a second embodiment partially installed in an opening in a heat eX- changer
  • Fig. 9 is a horizontal sectional view taken on the line 9--9 of Fig. 8;
  • Fig. 10 is a vertical sectional view taken on line 10--10 ofv Fig. 11 showing the device fully installed in the opening;
  • Fig. 11 is a horizontal sectional view taken on the line 11--11 of Fig. 10;
  • Fig. 12 is a perspective View of the secondcmbodiment in the locked position
  • Fig. 13 is a horizontal sectional View taken on the line lil-l of Fig. 8;
  • Fig. 14 is an elevational view of the safety pin portion of the second embodiment.
  • Fig. 1 one embodiment of the present invention. is generally indicated at l installed within similar openings or sockets 2 and 3 in the shell 4 of a heat exchanger generally indicated at 5.
  • the shell 4 also includesV a drain opening or connection 6 as well as inlet 7 and outlet 8.
  • a baflle plate 9 inclined from the inner surface of the shell 4.
  • the heat exchanger 5 also includes a head member 10 and a tube sheet 1l which form a headchamber 12.
  • a plurality or bundle of U-shaped heat exchanger tubes 13 having ends extending through and seated in the tube sheet 11 communicate with the head chamber 12.
  • the tubes 13 are supported in the shell 4 by a support plate 14 connected to the tube sheet by similar tie rods 15.
  • the head member lil is provided with an inlet 16 and an outlet 17.
  • the chamber 12 is divided into fluid-tight compartments by partition plates 18 and 19.
  • the open end 20 of the head member 1t) is closed by a removable Vhead cover 21.
  • the head member includes an opening or socket 22.
  • the heat exchanger 5 hydrostatically all but one of the openings and inlets are closed in a fluid-tight manner to seal the shell 4 during the test.
  • the inlet 7 and outlet 8 are provided with plates 23 which are secured in place by bolts 24 in a fluid-tight manner.
  • the test plugs 1 are readily installed as shown in Fig. 1. With all openings in the shell 4 closed, a water line 25' leading from a pressure pump (not shown) is connected to the opening 6 and the shell 4 is filled with water. Thereafter the pressure is applied to the water to test the connections between the tubes 13 and the tube sheet 11 hydrostatically.
  • the head member 10 is tested by closing the inlet 16 and the outlet 17 as well as other openings, such as the connection 22, and the seal between the head cover 21 and the open end 20 of the head member.
  • the head member 21 is sealed in place in a suitable manner.
  • the sockets 2, 3 and 22 have a bore 26 and an enlarged or countersunk portion 27 Yinto the bore 26.
  • the test plug 1 includes an elongated shaft 29, a positioning handle 30, an adjusting handle 31, a spacer 32, an annular gland 33, and a snap ring or member 34.
  • the shaft 29 has a threaded upper end portion 35, and the lower end is provided with a lug 36 which is preferably round.
  • the diameter of the lug 36 is greater thanA that of the shaft and less than that of the bore 26.
  • One side of the lug 36 is aligned with one side of the shaft 29 so that the center of the lug is offset to the left of the axis 38 of the shaft 29 as shown in Fig. 3.
  • the -lug 36 is eccentric of the shaft 29 with a crescent portion of the lug overlapping the lower end of the shaft.
  • the snap ring or member 34 is crescent-shaped and is rotatably mounted on a reduced or necked portion 39 of the shaft 29. As shown in Figs. 3 and 4, one side of the necked portion 39 is aligned with the aligned sides of the lug 36 and shaft 29, and the center 40 of the the ring 34 and the lug 36 so that upon insertion of the plug 1 into the socket 2 and rotation of the shaft 29, the lug clears the inner end of the socket.
  • the diameter of the 1ing.34 is greater than that of the shaft 29 and smaller than that of the bore 26, and preferably equal to the diameter of the lug 36.
  • the annular gland 33 has a diameter greater than that ofthe bore 26 and smaller than that of the countersunk portion 27.
  • the gland 36 is rotatably mounted on the shaft.
  • the gland 33 is movable longitudinally of the shaft 29.
  • the gland 33 has a bore 42 the center of which is aligned with the axis of the shaft 29 and offset from the axis 43 of the gland.
  • the outer .surface of the gland 33 includes a circumferential groove 44 in which is mounted an O-ring 45 of resilient or elastic material. As shown in Fig. 3 the ring 45 is seated in the groove 44 and its outer surface engages the wall of 'the countersunk portion 27 of the bore 26 when inserted therein.
  • the gland 33 includes a circumferential groove 46 around the bore 42 and an O-ring 47 of elastic material is disposed therein to provide a uid seal between the shaft 29 and the gland 33.
  • the gland 33 is also provided with a circumferential groove 48 on the outer surface above the groove 44. When the xture or plug 1 is properly inserted in the socket 2, the groove 48 is aligned with the outer end of the socket as shown in Fig. 5.
  • the spacer 32 is mounted on the shaft 29 between the gland 33 and the adjusting handle 31.
  • the spacer 32 is a cyclindrical member the lower end of which abuts the upper end of the gland 33 and the upper end of which abuts a nut 49 on the threaded portion 35 to which the handle 31 is attached.
  • the positioning handle 34 is fixedly mounted on the upper end of the shaft 29 by an annular member 50 that is seated over the upper end of the shaft 29.
  • the end of the handle 30 extends through the member 50 and engages an aligned aperture 29a in the shaft 29.
  • the fixture or plug 1 is manually inserted into the socket 2 with the various parts disposed as shown in Fig. 3; that is, the lug 36 and the ring 34 are aligned for insertion into the bore 26.
  • the adjusting handle 31 is in a withdrawn position on the threaded portion 35 so that the gland 33 may be inserted into the countersunk portion 27 with the ring 45 contacting the Walls of the countersunk portion.
  • the upper side of the lug 36 is clear of the inner end of the socket 22 by a distance preferably equal to the thickness of the shaft portion 41.
  • the snap ring 34 is entirely disposed within the bore 26.
  • the positioning handle 30 is aligned with a mark 52 on the upper end surface of the gland 33 as shown in Fig. 2.
  • the handle 30 After insertion, as shown in Fig. 5, the handle 30 is rotated until the shaft 29 contacts the wall of the bore 26.
  • the handle 30 may be rotated either clockwise or counterclockwise. Assuming the handle 30 is rotated counterclockwise the lug 36 rotates from the position of alignment with the snap ring 34 and the bore 26 (Fig. 3) to the position shown in Fig. 5. In the latter position a portion of the lug 36 overlaps the inner end of the socket 2 (Figs. 5 and 6). Thus, the plug 1 is clamped in place against the hydrostatic pressure created within the shell 4 during testing.
  • any fluid that may enter the bore 26 will be stopped at the O-rings 45 and 47.
  • the 0-ring 45 will be distorted between the socket 2 and the gland 33, as shown in Fig. 5.
  • the grooves 53 on the outer surface of the ring 34 enable iluid movement ⁇ into and out of the bore 26.
  • a second embodiment 54 is shown in Figs. 8, 10 and 12.
  • the second embodiment 54 is simllar -to the first in all respects except that the second embodiment is provided with a gland 55 of different construction from that of the gland 33.
  • the gland 55 is provided with a peripheral ange 56y which forms a ⁇ shoulder 57 that overlaps the upper end of the socket 2.
  • the shoulder 57 engages the outer end of the socket 2 surrounding the countersunk portion 27.
  • the gland 55 is provided with a peripheral groove 58 -in its outer surface and a groove 59 surrounding the shaft 29.
  • the O-rings 60 and 61 are seated in the grooves 58 and 59, respectively.
  • the test plug 54 is provided with la safety pin 62 as shown in lFig. 12.
  • the test plug 54 also includes the elongated shaft 29, the positioning handle 30, the adjusting handle 31, the spacer 32, and the snap ring 34.
  • the shaft 29 has a threaded upper end portion 35 and the lower end is provided with the lug 36.
  • the gland 55 has an upper surface 63 (Figs. 12 and 13) in which a number of marks are inscribed including a mark 64, a mark 65, and a mark 66, which denote respectively the unlocked position, the position of minimum lock, and the position of maximum lock of the positioning handle 30. Between the marks 65 and 66 is the safe lock position.
  • the positioning handle 30 is aligned with the mark 64 so that the central or larger portion of the crescent-shaped lug 36 and the gland 55 are aligned with each other.
  • the positioning handle 30 may be rotated either clockwise or counterclockwise. However, the preferred direction of rotation is clockwise, or to the left from the position shown in Fig. 8 to that of Fig. 101.
  • the snap ring 34 and the shaft 29 expand radially from their -compact position (Fig. 8) to the expanded position (Fig. l) and engage approximate diametrically opposite sides of the bore 26 of the socket 2.
  • the initial and final positions of the lug 36, the snap ring 34 and the shaft 29 are shown, respectively, in Figs. 9 and ll.
  • the handle 30 In the locked position the handle 30 must be disposed between the marks 65 and 66 (Figs. 12 .and 13) which denote the positions of minimum and maximum overlap of the lug 36 with the inner end of the socket 2. Thereafter, the adjusting handle 3l is rotated clockwise in order yto draw the upper surface of the lug 36 into engagement with the lower end of the socket 2 ⁇ as well as to seat the gland 5S into the countersunk portion 27 of the bore 26.
  • frictional forces between spacer 32, the gland 55, and the shaft 29 urge the shaft 29 to rotate slightly in the same direction if not restrained.
  • the positioning handle 39 by rotating the positioning handle 39 clockwise, rather than counterclockwise, the subsequent clockwise rotation of the .adjusting handle -31 urges the positioning handle 3i) to retain its location in the safe lock position between the marks 65 and 66.
  • the upper surface 63 -of the gland 55 at the mark 65 is provided with a threaded aperture 67 adapted to receive a lower threaded end 6&3 of the pin 62.
  • the safety pin 62 having an outturned upper end 69, is inserted into the threaded aperture 67 from which it extends upwardly above ⁇ the handle 30.
  • the present invention provides a new land useful test plug for heat exchangers by which heat exchangers or other pressure vessels may be subjected to hydrostatic pressures before shipping the heat exchanger to a customer.
  • the test plug when properly installed is selfsealing. It is quickly attached and removed from an outlet. Moreover, it may be used repeatedly and is not expended with repeated usage.
  • a testV plug for sealing .an aperture in the wall of va pressure-vessel including Ia plug shaft, a laterally extending lug on one end of the shaft having a lateral dimension smaller than that .of the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, the ⁇ shafthav-ing a necked portion of smaller diameter thany the shaft intermediate the lug and gland, a crescentshaped member rotatably mounted on the shaft necked portion, the member having an outer diameter ⁇ smaller than that ⁇ of the aperture, O-ring means mounted on the gland, and means on the shaft for slideably moving the gland tow-ard thecrescent-shaped member and lug.
  • a ftest plug for sealing an laperture in the wall of a pressure-vessel including a plug shaft, a round lug eccentrically mounted on one end of the shaft having a diameter greater than the shaft diameter and smaller than that of the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, the shaft having a necked portion of smaller diameter than the shaft, ⁇ the axis of the necked portion being eccentric to the shaft axis, a member having an inner circular surface journaled on the shaft necked portion, the member having an outer diameter eccentric to its inner surface and smaller than that of the aperture, the member being located intermediate the lug and gland, the gland being provided With a portion adapted for engagement with a pressure-vessel wall portion when slideably moved along the shaft, O-ring means on the gland for sealing the gland in an aperture in which the test plug is inserted, and means on the shaft for slideably moving the gland toward the lug to clamp the test plug to a pressure-vessel wall between the gland and lug when inserted
  • vA test plug for sealing an aperture in the wall of a pressure-vessel, including a plug shaft, a laterally extending lug on one end of the shaft having a lateral dimension smaller than that of the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, the shaft having a necked portion of smaller diameter than the shaft, a member having an inner circular surface journaled on the shaft necked portion, the member having 'an outer diameter eccentric to its inner surface and smaller than that of the aperture, the member being located intermediate the lug and gland, the gland being provided with a portion adapted for engagement with ia pressure-vessel wall portion when slideably moved along the shaft, O-ring means on the gland for sealing the gland in an aperture in which the test plug is inserted, and means on the shaft for slideably moving the gland toward the lug to clamp the test plug to a pressure-vessel Wall between the gland and lug when inserted in la wall aperture to be sealed.
  • Test plug closure construction for sealing an yaperture in the wall of a pressure-vessel, including ya vessel wall portion having an aperture, an enl-arged countersunk shoulder portion formed in the vessel wall surrounding and communicating with the aperture, a plug shaft extending through the countersunk portion and apertui'e, a laterally extending lug on one end of the shaft having a lateral dimension smaller than that of the aperture movable to a position engaging the wall beneath the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, a member having an inner circular surface journaled on the shaft, the member having an outer diameter eccentric to its inner surface and smaller than that of the aperture, the member being located in the aperture and intermediate the lug and the gland, at least a portion of the gland being received in the enlarged countersunk pressure-vessel wall portion, O-ring means sealing .the joint between the gland and the countersunk pressure-Vessel Wall portion, means for turning the shaft when inserted in the aperture relative thereto to engage
  • Test plug closure construction for sealing an aperture -in the wall of a pressure vessel, including a vessel wall portion provided with an aperture, the apertureforming wall portion being provided with a countersunk annular shoulder intermediate the inner and outer cylindrioal ends of the aperture and forming an enlarged aperture portion between the shoulder and outer end of the aperture and a smaller aperture portion between the shoulder and inner end of the aperture, a cylindrical gland sleeve seated against a portion ⁇ of the vessel wall and extending within the enlarged aperture portion, O-ring means sealing the joint between the gland sleeve and the enlarged aperture portion, shaft means extending through the gland sleeve and aperture and eccentrically located with respect to each, laterally extending lug means on one end of the shaft means, the shaft means being axially slidable and rotatable with respect tol the gland sleeve, the laterally extending portion of the lug means being movable when the shaft means is rotated with respect to the gland sleeve between a position radially

Description

` May 28, 1957 R. l.. MclNNEs 2,793,784
TEST PLUG FOR PRESSURE VESSELS Filed Feb. '7, 1956 2 Sheets-Sheet l l y Rbr BY Qw May 28, 1957 R. L. MCINNS 2,793,784
I TEST PLUG FOR PRESSURE VESSELS Filed Feb. '7, 1956 Sheets-Sheet 2 my 14 *i 1N V EN TOR.
TTORNEYS United Star TEST PLUG FR PRESSURE VESSELS Application February 7, 1956, Serial No. 564,017
17 Claims. (Cl. 220-25) This invention relates to a test plug and more pa-rticularly it pertains to a quick opening closure for openings in a heat exchanger for testing purposes.
Heat exchangers are provided with inlets and outlets for the passage of heat exchange fluids as well as other openings for various other purposes. Such openings are usually used for the connection of instruments, such as gage glasses and pressure valves.
Most heat exchangers built in accordance with construction lcodes Iare hydrostatically tested to insure the tightness of gasketed joints and to prove the mechanical integrity of the design. A test pressure at least equal to one and one-half times the design pressure is usually required by construction codes. In order to apply the test pressures all openings must be closed of, except one opening through which the test tiuid is pumped into the pressure vessel.
In the past these openings, lacking threads or other attaching means, were closed off for testing by welding a plug into the opening, or by welding lugsl on the outside ofthe connection to which a clamp is attached for holding a gasket plate in place. After the test, the plug or lugs `and gasket plate are removed and the residue of the welds removed by grinding to restore the outer surface.
Inasmuch as the foregoing procedure for closing openings in a heat exchanger or pressure vessel was time,- consuming and wasteful of materials, it was desirable to provide a substitute means for closing the openings of the heat exchangers for pressure testing.
I have discovered a self-sealing device for closing openings in a heat exchanger which is quickly and easily installed and removed manually without the use of tools. The device is adapted to operate at all testing pressures for heat exchangers.
Accordingly, it is a general object of this invention to provide a test plug for openings in a heat exchanger that is quickly and easily installed and removed.
It is another object of this invention to provide a test plug for the openings in a heat exchanger that is self-sealing.
Another object of this invention is to provide a test plug for the -openings in a heat exchanger that is manually operated without the aid of tools.
Finally, it is an object of this invention to provide an improved test plug for heat exchangers which incorporates the foregoing desiderata in an inexpensive manner.
These and other objects apparent to those skilled in the art from the foregoing description and claims may be obtained, the stated results achieved and described difculties overcome by the discoveries, principles, apparatus, parts, combinations, subcombinations and elements which comprise the present invention, the nature of which is set forth in the following statement, preferred embodiments of which-illustrative of the best modes in which applicant has contemplated applying arent .2,793,784 Patented May 28, 1957 the principles-are set forth in the following description, and which are particularly and distinctly pointed out and set forth in the appended claims forming part thereof.
The nature of the improvedv test plug construction of the present invention may be stated in general terms as including a shaft having a threaded end and having a lug at the other end, the lug having a lateral dimension greater than the diameter of the shaft and smaller than the diameter of tne opening in a pressure vessel. In addition, a necked portion is provided on the shaft adjacent the lug, and a crescent-shaped snap ring is rotatably mounted on the necked portion having a diameter less than that of the opening. An annular member is rotatably mounted on the shaft between the necked portion and the threaded end, the member having a portion of diameter smaller than that of the pressurevessel opening and having a circumferential groove around said portion with a resilient gasket partially seated therein for engagement with the opening, and a nut mounted on the threaded end of the shaft for tightening the assembly in the opening.
The preferred embodiments of the invention areillustrated, by way of example, in the accompanying drawings wherein:
Fig. 1 is a vertical sectional View through a heat exchanger showing one embodiment of the present invention installed therein;
Fig. 2 is a perspective view of the device;
Fig. 3 is a vertical sectional view showing thedevice partially installed in an opening in a heat exchanger;
Fig. 4 is a horizontal sectional View taken on the line 4-4 of Fig. 3;
Fig. 5 is a vertical sectional view showing the device fully installed in the opening;
Fig. 6 is a horizontal sectional view taken on the line 6-6 of Fig. 5;
Fig. 7 is a horizontal sectional View taken on the line 7-7' of Fig. 5;
Fig. 8 is a vertical sectional view of a second embodiment partially installed in an opening in a heat eX- changer;
Fig. 9 is a horizontal sectional view taken on the line 9--9 of Fig. 8;
Fig. 10 is a vertical sectional view taken on line 10--10 ofv Fig. 11 showing the device fully installed in the opening;
Fig. 11 is a horizontal sectional view taken on the line 11--11 of Fig. 10;
Fig. 12 is a perspective View of the secondcmbodiment in the locked position;
Fig. 13 is a horizontal sectional View taken on the line lil-l of Fig. 8; and
Fig. 14 is an elevational view of the safety pin portion of the second embodiment.
Similar numerals refer to similar parts throughout the various gures of the drawings. i
In Fig. 1 one embodiment of the present invention. is generally indicated at l installed within similar openings or sockets 2 and 3 in the shell 4 of a heat exchanger generally indicated at 5. The shell 4 also includesV a drain opening or connection 6 as well as inlet 7 and outlet 8. Below the inlet 7 is a baflle plate 9 inclined from the inner surface of the shell 4.
The heat exchanger 5 also includes a head member 10 and a tube sheet 1l which form a headchamber 12. A plurality or bundle of U-shaped heat exchanger tubes 13 having ends extending through and seated in the tube sheet 11 communicate with the head chamber 12. The tubes 13 are supported in the shell 4 by a support plate 14 connected to the tube sheet by similar tie rods 15.
The head member lil is provided with an inlet 16 and an outlet 17. The chamber 12 is divided into fluid-tight compartments by partition plates 18 and 19. The open end 20 of the head member 1t) is closed by a removable Vhead cover 21. Moreover, the head member includes an opening or socket 22.
To' test the heat exchanger 5 hydrostatically all but one of the openings and inlets are closed in a fluid-tight manner to seal the shell 4 during the test. In addition, the inlet 7 and outlet 8 are provided with plates 23 which are secured in place by bolts 24 in a fluid-tight manner. For the smaller openings or sockets 2 and 3 the test plugs 1 are readily installed as shown in Fig. 1. With all openings in the shell 4 closed, a water line 25' leading from a pressure pump (not shown) is connected to the opening 6 and the shell 4 is filled with water. Thereafter the pressure is applied to the water to test the connections between the tubes 13 and the tube sheet 11 hydrostatically.
In a similar manner the head member 10 is tested by closing the inlet 16 and the outlet 17 as well as other openings, such as the connection 22, and the seal between the head cover 21 and the open end 20 of the head member. The head member 21 is sealed in place in a suitable manner.
. As shown in Figs. 3 and 5 the sockets 2, 3 and 22 have a bore 26 and an enlarged or countersunk portion 27 Yinto the bore 26. The test plug 1 includes an elongated shaft 29, a positioning handle 30, an adjusting handle 31, a spacer 32, an annular gland 33, and a snap ring or member 34. The shaft 29 has a threaded upper end portion 35, and the lower end is provided with a lug 36 which is preferably round. The diameter of the lug 36 is greater thanA that of the shaft and less than that of the bore 26. One side of the lug 36 is aligned with one side of the shaft 29 so that the center of the lug is offset to the left of the axis 38 of the shaft 29 as shown in Fig. 3. Hence, the -lug 36 is eccentric of the shaft 29 with a crescent portion of the lug overlapping the lower end of the shaft.
The snap ring or member 34 is crescent-shaped and is rotatably mounted on a reduced or necked portion 39 of the shaft 29. As shown in Figs. 3 and 4, one side of the necked portion 39 is aligned with the aligned sides of the lug 36 and shaft 29, and the center 40 of the the ring 34 and the lug 36 so that upon insertion of the plug 1 into the socket 2 and rotation of the shaft 29, the lug clears the inner end of the socket. The diameter of the 1ing.34 is greater than that of the shaft 29 and smaller than that of the bore 26, and preferably equal to the diameter of the lug 36.
The annular gland 33 has a diameter greater than that ofthe bore 26 and smaller than that of the countersunk portion 27. Like the ring 34, the gland 36 is rotatably mounted on the shaft. Moreover, the gland 33 is movable longitudinally of the shaft 29. The gland 33 has a bore 42 the center of which is aligned with the axis of the shaft 29 and offset from the axis 43 of the gland. The outer .surface of the gland 33 includes a circumferential groove 44 in which is mounted an O-ring 45 of resilient or elastic material. As shown in Fig. 3 the ring 45 is seated in the groove 44 and its outer surface engages the wall of 'the countersunk portion 27 of the bore 26 when inserted therein.
In addition, the gland 33 includes a circumferential groove 46 around the bore 42 and an O-ring 47 of elastic material is disposed therein to provide a uid seal between the shaft 29 and the gland 33. The gland 33 is also provided with a circumferential groove 48 on the outer surface above the groove 44. When the xture or plug 1 is properly inserted in the socket 2, the groove 48 is aligned with the outer end of the socket as shown in Fig. 5.
The spacer 32 is mounted on the shaft 29 between the gland 33 and the adjusting handle 31. The spacer 32 is a cyclindrical member the lower end of which abuts the upper end of the gland 33 and the upper end of which abuts a nut 49 on the threaded portion 35 to which the handle 31 is attached.
The positioning handle 34) is fixedly mounted on the upper end of the shaft 29 by an annular member 50 that is seated over the upper end of the shaft 29. The end of the handle 30 extends through the member 50 and engages an aligned aperture 29a in the shaft 29.
The fixture or plug 1 is manually inserted into the socket 2 with the various parts disposed as shown in Fig. 3; that is, the lug 36 and the ring 34 are aligned for insertion into the bore 26. In addition, the adjusting handle 31 is in a withdrawn position on the threaded portion 35 so that the gland 33 may be inserted into the countersunk portion 27 with the ring 45 contacting the Walls of the countersunk portion. Thus, in the position shown in Fig. 3 the upper side of the lug 36 is clear of the inner end of the socket 22 by a distance preferably equal to the thickness of the shaft portion 41. Also, the snap ring 34 is entirely disposed within the bore 26. Moreover, the positioning handle 30 is aligned with a mark 52 on the upper end surface of the gland 33 as shown in Fig. 2.
After insertion, as shown in Fig. 5, the handle 30 is rotated until the shaft 29 contacts the wall of the bore 26. The handle 30 may be rotated either clockwise or counterclockwise. Assuming the handle 30 is rotated counterclockwise the lug 36 rotates from the position of alignment with the snap ring 34 and the bore 26 (Fig. 3) to the position shown in Fig. 5. In the latter position a portion of the lug 36 overlaps the inner end of the socket 2 (Figs. 5 and 6). Thus, the plug 1 is clamped in place against the hydrostatic pressure created within the shell 4 during testing.
During the rotation of the lug 36 to the position shown in Fig. 5, the portion of the shaft 29 between the necked portion and the shoulder 28 moves into contact with the wall of the bore 26. Continued rotation of the shaft 29 drives the snap ring 34 against the side of the bore 26 diametrically opposite the contact point of the shaft. During the rotation of the shaft 29, the axis 40 of the necked portion 39 moves with respect to the axis 38 of the shaft 29 (see Figs. 4 and 6). Further rotation of the shaft 29 is inhibited by the camming and binding action between the parts thereby limiting the rotation of the lug 36 to less than 180 counterclockwise from the initial position of Figs. 2, 3 and 4.
Thereafter the handle 31 is rotated clockwise until the lower end of the gland 33 is seated against the shoulder 28, pulling the shaft 29 longitudinally upwardly as shown in Fig. 5 until the overlapping portion of the lug 36 engages the corresponding portion of the end of the lsocket 2. In the latter position the plug 1 is sealed in place within the socket 2.
When the shell 4 is tested hydrostatieally by a suitable fluid, such yas water, any fluid that may enter the bore 26 will be stopped at the O- rings 45 and 47. The 0-ring 45 will be distorted between the socket 2 and the gland 33, as shown in Fig. 5. The grooves 53 on the outer surface of the ring 34 enable iluid movement `into and out of the bore 26.
:In `addition to the embodiment of the invention shown in Figs. 1 to 7, a second embodiment 54 is shown in Figs. 8, 10 and 12. The second embodiment 54 is simllar -to the first in all respects except that the second embodiment is provided with a gland 55 of different construction from that of the gland 33. The gland 55 is provided with a peripheral ange 56y which forms a `shoulder 57 that overlaps the upper end of the socket 2. As shown in Fig. l0, when the test plug 54 is completely installed, the shoulder 57 engages the outer end of the socket 2 surrounding the countersunk portion 27. In addition, the gland 55 is provided with a peripheral groove 58 -in its outer surface and a groove 59 surrounding the shaft 29. The O- rings 60 and 61 are seated in the grooves 58 and 59, respectively. In addition, the test plug 54 is provided with la safety pin 62 as shown in lFig. 12.
As in the test plug 1 of Figs. 1-7, the test plug 54 also includes the elongated shaft 29, the positioning handle 30, the adjusting handle 31, the spacer 32, and the snap ring 34. The shaft 29 has a threaded upper end portion 35 and the lower end is provided with the lug 36.
The gland 55 has an upper surface 63 (Figs. 12 and 13) in which a number of marks are inscribed including a mark 64, a mark 65, and a mark 66, which denote respectively the unlocked position, the position of minimum lock, and the position of maximum lock of the positioning handle 30. Between the marks 65 and 66 is the safe lock position. When the test plug 54 is inserted into the socket 2 the positioning handle 30 is aligned with the mark 64 so that the central or larger portion of the crescent-shaped lug 36 and the gland 55 are aligned with each other.
As was set forth with respect to the test plug 1 of the invention, the positioning handle 30 may be rotated either clockwise or counterclockwise. However, the preferred direction of rotation is clockwise, or to the left from the position shown in Fig. 8 to that of Fig. 101. Upon rotating the positioning handle 30 inthe clockwise direction from its position of alignment with the mark 64, the snap ring 34 and the shaft 29 expand radially from their -compact position (Fig. 8) to the expanded position (Fig. l) and engage approximate diametrically opposite sides of the bore 26 of the socket 2. The initial and final positions of the lug 36, the snap ring 34 and the shaft 29 are shown, respectively, in Figs. 9 and ll.
In the locked position the handle 30 must be disposed between the marks 65 and 66 (Figs. 12 .and 13) which denote the positions of minimum and maximum overlap of the lug 36 with the inner end of the socket 2. Thereafter, the adjusting handle 3l is rotated clockwise in order yto draw the upper surface of the lug 36 into engagement with the lower end of the socket 2 `as well as to seat the gland 5S into the countersunk portion 27 of the bore 26. During the clockwise rotation of the adjusting handle 3l on vthe threaded end portion 3S of the shaft 29 frictional forces between spacer 32, the gland 55, and the shaft 29 urge the shaft 29 to rotate slightly in the same direction if not restrained. Hence, by rotating the positioning handle 39 clockwise, rather than counterclockwise, the subsequent clockwise rotation of the .adjusting handle -31 urges the positioning handle 3i) to retain its location in the safe lock position between the marks 65 and 66. In addition, the upper surface 63 -of the gland 55 at the mark 65 is provided with a threaded aperture 67 adapted to receive a lower threaded end 6&3 of the pin 62.
To prevent the handle from rotating counterclockwise beyond the mark 65 `the safety pin 62, having an outturned upper end 69, is inserted into the threaded aperture 67 from which it extends upwardly above `the handle 30.
The present invention provides a new land useful test plug for heat exchangers by which heat exchangers or other pressure vessels may be subjected to hydrostatic pressures before shipping the heat exchanger to a customer. The test plug when properly installed is selfsealing. It is quickly attached and removed from an outlet. Moreover, it may be used repeatedly and is not expended with repeated usage. Y
In the foregoing description certain terms have been used for brevity, clearness and understanding,`but no unnecessary limitations are to be implied therefrom beyond the requirements ofl the prior art, because such words are used for descriptive purposes herein and are intended to be broadly construed.
Moreover, the embodiments of the improved construction illustratedA and described herein are by way of example and the scope of the present invention is not limited to `the exact. details of construction shown.
Having now described the features, construction and principles of the invention, the characteristic of the test plug construction, and the advantageous, new and useful results provided; the new and useful discoveries, principles, parts, elements, combinations, subcombinations, structures and arrangements and mechanical equivalents thereof obvious to those skilled in the art, are set forth in the appended claims.
II claim:
1. A testV plug for sealing .an aperture in the wall of va pressure-vessel, including Ia plug shaft, a laterally extending lug on one end of the shaft having a lateral dimension smaller than that .of the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, the `shafthav-ing a necked portion of smaller diameter thany the shaft intermediate the lug and gland, a crescentshaped member rotatably mounted on the shaft necked portion, the member having an outer diameter `smaller than that `of the aperture, O-ring means mounted on the gland, and means on the shaft for slideably moving the gland tow-ard thecrescent-shaped member and lug.
2. The construction defined in claim 1 in which the shaft necked portion is located adjacent the lug.
3. The construction defined in claim 1 in which the means for moving the gland includes a nut adjustable on the shaft.
4. The construction defined in claim l in which the sha-ft is provided with handle means for inserting the shaft, the lug, the crescent-shaped member, and the sleeve in an aperture to be sealed, and for rotating the lug with respect to the aperture and the crescent-shaped member; and said gland-moving means being adapted to move the gland toward the lug and 4the cla-mp pressurevessel wall portions surrounding the aperture between the lug and the gland.
5. The construction defined in claim l in which indicator means are provided on the shaft and the gland which are -aligned for insertion of the plug in an aperture to be sealed, and in which 4the shaft and gland indicator means are rotated relative to one another to establish lug engagement with a pressure-vessel wall when the test plug is inserted in a wall aperture to be sealed.
6. The construction defined in claim 5 in which other indicator means are provided on the gland which may be aligned with said shaft indicator means upon relative rotation between the shaft and gland to engage a test plug in an laperture to be sealed, and in which lug engagement with a pressure-vessel wall in a safe manner is established when said other indicator means and said shaft indicator means are aligned.
7. The construction defined in claim 6 in which disengageable locking means is provided between the shaft and the gland preventing relative unlocking rotation between the shaft and gland after a locked position of the parts has been established.
8. The construction defined in claim l in which O-ring sealing means is provided between the shaft and gland.
9. A ftest plug for sealing an laperture in the wall of a pressure-vessel, including a plug shaft, a round lug eccentrically mounted on one end of the shaft having a diameter greater than the shaft diameter and smaller than that of the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, the shaft having a necked portion of smaller diameter than the shaft, `the axis of the necked portion being eccentric to the shaft axis, a member having an inner circular surface journaled on the shaft necked portion, the member having an outer diameter eccentric to its inner surface and smaller than that of the aperture, the member being located intermediate the lug and gland, the gland being provided With a portion adapted for engagement with a pressure-vessel wall portion when slideably moved along the shaft, O-ring means on the gland for sealing the gland in an aperture in which the test plug is inserted, and means on the shaft for slideably moving the gland toward the lug to clamp the test plug to a pressure-vessel wall between the gland and lug when inserted in a wall aperture to be sealed.
10. vA test plug for sealing an aperture in the wall of a pressure-vessel, including a plug shaft, a laterally extending lug on one end of the shaft having a lateral dimension smaller than that of the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, the shaft having a necked portion of smaller diameter than the shaft, a member having an inner circular surface journaled on the shaft necked portion, the member having 'an outer diameter eccentric to its inner surface and smaller than that of the aperture, the member being located intermediate the lug and gland, the gland being provided with a portion adapted for engagement with ia pressure-vessel wall portion when slideably moved along the shaft, O-ring means on the gland for sealing the gland in an aperture in which the test plug is inserted, and means on the shaft for slideably moving the gland toward the lug to clamp the test plug to a pressure-vessel Wall between the gland and lug when inserted in la wall aperture to be sealed.
1l.. The construction defined in claim 10 in which the end o'f the gland nearest the lug constitutes the portion adapted for engagement with a pressure-vessel wall portion.
12. The construction defined in claim in which the gland is provided with an annular shoulder, and in which the shoulder comprises the portion of the gland adapted for engagement with a pressure-vessel wall portion.
13. The construction defined in claim 10 in which the axis of the necked portion is eccentric to the shaft axis, and in which the axis of the necked portion is offset from that of the shaft in a different direction from the offset of the lateral extent of the lug from the axis of the shaft.
14. Test plug closure construction for sealing an yaperture in the wall of a pressure-vessel, including ya vessel wall portion having an aperture, an enl-arged countersunk shoulder portion formed in the vessel wall surrounding and communicating with the aperture, a plug shaft extending through the countersunk portion and apertui'e, a laterally extending lug on one end of the shaft having a lateral dimension smaller than that of the aperture movable to a position engaging the wall beneath the aperture, a gland sleeve slideable and eccentrically journaled on the shaft, a member having an inner circular surface journaled on the shaft, the member having an outer diameter eccentric to its inner surface and smaller than that of the aperture, the member being located in the aperture and intermediate the lug and the gland, at least a portion of the gland being received in the enlarged countersunk pressure-vessel wall portion, O-ring means sealing .the joint between the gland and the countersunk pressure-Vessel Wall portion, means for turning the shaft when inserted in the aperture relative thereto to engage the lug with the vessel wall portion beneath the aperture, and means on the shaft for moving the sleeve into the vessel wail countersunk portion and for maintaining the same therein when the lug is engaged with the vessel wall.
l5. The construction defined in claim 14 in which the shaft is provided with means for moving the member and the shaft relative to the aperture and to each other to laterally clamp the member and shaft against the wall of the aperture.
16, Test plug closure construction for sealing an aperture -in the wall of a pressure vessel, including a vessel wall portion provided with an aperture, the apertureforming wall portion being provided with a countersunk annular shoulder intermediate the inner and outer cylindrioal ends of the aperture and forming an enlarged aperture portion between the shoulder and outer end of the aperture and a smaller aperture portion between the shoulder and inner end of the aperture, a cylindrical gland sleeve seated against a portion `of the vessel wall and extending within the enlarged aperture portion, O-ring means sealing the joint between the gland sleeve and the enlarged aperture portion, shaft means extending through the gland sleeve and aperture and eccentrically located with respect to each, laterally extending lug means on one end of the shaft means, the shaft means being axially slidable and rotatable with respect tol the gland sleeve, the laterally extending portion of the lug means being movable when the shaft means is rotated with respect to the gland sleeve between a position radially within the circumference of the smaller aperture portion iand a second position extending radially beyond the circumference of the smaller aperture portion, means on the shaft for slidably moving the lng means toward the gland sleeve when the latter is seated against a vessel wall portion, and said lug means when in said second position engaging the vessel wall at the inner end of the aperture when the lug means is moved by said moving means to clamp the vessel wall between the gland and lug means to seal the aperture.
17. The construction defined in claim 16 in which O-ring sealing means is provided for the slidable and rotatable joint between the shaft means and gland.
References Cited in the le of this patent UNITED STATES PATENTS 63,706 Crompton Apr. 9, 1867 1,296,275 Firth Mar. 4, 1919 1,684,983 Clark Sept. 18, 1928 2,581,536 Johns Jan. 8, 1952 2,581,537 Maisch Jan. 8, 1952 2,683,499 De Croes July 13, 1954 2,705,574 Schoessow et al. Apr. 5, 1955
US564017A 1956-02-07 1956-02-07 Test plug for pressure vessels Expired - Lifetime US2793784A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938646A (en) * 1958-01-07 1960-05-31 Babcock & Wilcox Co Closure plugs
US3896902A (en) * 1974-05-30 1975-07-29 Us Air Force Plug for drive shaft with internal drive spline

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US63706A (en) * 1867-04-09 Improvement in bolts asd bolt-heads
US1296275A (en) * 1918-10-21 1919-03-04 William C Firth Holding device.
US1684983A (en) * 1927-11-26 1928-09-18 Horace W Clark Box or casing cover with fastener
US2581537A (en) * 1949-07-19 1952-01-08 Rheem Mfg Co Self-sealing test plug
US2581536A (en) * 1946-10-07 1952-01-08 Rheem Mfg Co Self-sealing test plug
US2683499A (en) * 1949-02-26 1954-07-13 Croes Leon C De Drain-controlling device
US2705574A (en) * 1950-08-01 1955-04-05 Babcock & Wilcox Co Laminated binder for handhole closure fitting

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US63706A (en) * 1867-04-09 Improvement in bolts asd bolt-heads
US1296275A (en) * 1918-10-21 1919-03-04 William C Firth Holding device.
US1684983A (en) * 1927-11-26 1928-09-18 Horace W Clark Box or casing cover with fastener
US2581536A (en) * 1946-10-07 1952-01-08 Rheem Mfg Co Self-sealing test plug
US2683499A (en) * 1949-02-26 1954-07-13 Croes Leon C De Drain-controlling device
US2581537A (en) * 1949-07-19 1952-01-08 Rheem Mfg Co Self-sealing test plug
US2705574A (en) * 1950-08-01 1955-04-05 Babcock & Wilcox Co Laminated binder for handhole closure fitting

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938646A (en) * 1958-01-07 1960-05-31 Babcock & Wilcox Co Closure plugs
US3896902A (en) * 1974-05-30 1975-07-29 Us Air Force Plug for drive shaft with internal drive spline

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